Reusable mechanically fused dovetail retainer mechanisms

ABSTRACT

A reusable mechanism is disclosed for coupling two robotic appendages, such that an unintended force acting against a side of one of the appendages may decouple the appendages. The mechanism includes a revolved male dovetail mated to a revolved female dovetail. The mechanism may further include a channel within the male dovetail and a detent that inhibits rotation of the male dovetail in relation to the female dovetail.

BACKGROUND

As technology advances, various types of robotic devices are beingcreated for performing a variety of functions that may assist users.Robotic devices may be used for applications involving materialhandling, transportation, welding, assembly, and dispensing, amongothers. Over time, the manner in which these robotic systems operate isbecoming more intelligent, efficient, and intuitive. As robotic systemsbecome increasingly prevalent in numerous aspects of modern life, it isdesirable for robotic systems to be efficient. Therefore, a demand forefficient robotic systems has helped open up a field of innovation inactuators, movement, sensing techniques, as well as component design andassembly.

Robotic devices, such as robotic legs and arms, may include variouscomponents or attachments that are designed to interact with theenvironment. Such components may include robotic feet and hands, whichmay include additional components that can be used to support,stabilize, grip, and otherwise allow a robotic device to effectivelycarry out one or more actions.

In particular, robotic arms may include one or more “end effectors” thatinteract with the environment. For example, end effectors may beimpactive (such as a claw), enveloping, ingressive (such as a pin orneedle), astrictive (such as a vacuum or suction element) or contigutive(requiring contact for adhesion, such as glue).

SUMMARY

The present application discloses implementations of a system andmechanism for coupling two robotic appendages (e.g., a finger and anactuator base), such that an unintended force acting against a side ofone of the appendages decouples the appendages. Further, the mechanismis not damaged or destroyed during the decoupling and the appendages maybe recoupled together via the mechanism. In practical effect, themechanism acts as a mechanical fuse between the appendages.

In one example, the present application describes a retainer mechanismthat includes a first member and a second member. The first member mayinclude a first body and a male dovetail extending outward from thefirst body. The male dovetail may include two outer surfaces inclinedrelative to each other and the male dovetail may be arranged in an arcabout a central axis. The second member may include a second body and afemale dovetail extending outward from the second body. The femaledovetail may include two inner surfaces inclined relative to each otherthat define a first channel between the two inner surfaces. The femaledovetail may be arranged in an arc about the central axis and beconfigured to couple with the male dovetail, such that each of the twoouter surfaces of the male dovetail mates with one of the respectiveinner surface of the female dovetail.

In another example, the present application describes a robotic systemthat includes a retainer mechanism, a first robotic appendage, and asecond robotic appendage. The retainer mechanism includes a first memberand a second member. The first member may include a male dovetailstructure arranged in an arc about a central axis, and the second membermay include a female dovetail structure arranged in an arc about thecentral axis. The first member may be coupled to the second member viathe male and female dovetail structures. The first robotic appendage maybe fixedly coupled to either the first or second member of the retainer.The second robotic appendage may be fixedly coupled to the member notfixedly coupled to the first robotic appendage. The retainer mechanismmay be configured to allow the first member to decouple from the secondmember via the male and female dovetail structures when a force appliedto a side of the first robotic appendage is more than a threshold force.

In another example, the present application describes a retainermechanism that includes a first member, a second member, and a detent.The first member may include a first body and a male dovetail extendingoutward from the first body. The male dovetail may include two outersurfaces inclined relative to each other with an inner channel locatedbetween the two outer surfaces. The male dovetail may be arranged in anarc about a central axis. The second member may include a second bodyand a female dovetail extending outward from the second body. The femaledovetail may include two inner surfaces inclined relative to each otherthat define a first channel between the two inner surfaces. The femaledovetail may be arranged in an arc about the central axis and beconfigured to couple with the male dovetail, such that each of the twoouter surfaces of the male dovetail mates with one of the respectiveinner surface of the female dovetail. The detent may be configured toinhibit rotational movement of the first body relative to the secondbody about the central axis.

The foregoing summary is illustrative only and is not intended to be inany way limiting. In addition to the illustrative aspects, embodiments,and features described above, further aspects, embodiments, and featureswill become apparent by reference to the figures and the followingdetailed description and the accompanying drawings.

BRIEF DESCRIPTION OF THE FIGURES

FIG. 1 illustrates a configuration of a robotic system, according to anexample implementation.

FIG. 2 illustrates an example robotic arm system, according to anexample implementation.

FIG. 3 illustrates an example gripper, according to an exampleembodiment.

FIGS. 4A and 4B illustrate side and perspective views, respectively, ofan example retainer mechanism, according to an example implementation.

FIGS. 4C and 4D illustrate perspective and side section views,respectively, of an example retainer mechanism, according to an exampleimplementation

FIGS. 4E-G illustrate top, front, and perspective views, respectively,of retainer mechanism components, according to an exampleimplementation.

FIGS. 4H and 4I illustrate perspective views of retainer mechanismcomponents, according to an example implementation.

FIGS. 4J and 4K illustrate perspective views and bottom views,respectively, of a retainer mechanism component, according to an exampleimplementation.

FIGS. 5A-C illustrate a step-wise coupling of a retainer mechanism,according to an example implementation.

FIG. 6 illustrates a retainer mechanism during side-force decoupling,according to an example implementation.

FIG. 7 illustrates reference dimensions of a retainer mechanism,according to an example implementation.

FIG. 8 is a chart illustrating Root Width versus Fuse-out Force andSafety Factor, according to an example implementation.

FIG. 9 is a chart illustrating Fuse-out Force versus Fuse-out Cycles,according to an example implementation.

FIGS. 10A and 10B illustrate front and perspective views, respectively,of a retainer mechanism and insert, according to an exampleimplementation.

FIG. 11 is a chart illustrating Fuse-out Force versus Fuse-out Cycles,according to an example implementation.

FIGS. 12 and 13 illustrate alternative detent locations, according toexample implementations.

DETAILED DESCRIPTION

The following detailed description describes various features andfunctions of the disclosed devices, systems, and methods with referenceto the accompanying figures. The illustrative device, system, and methodembodiments described herein are not meant to be limiting. It should beunderstood that the words “exemplary,” “example,” and “illustrative,”are used herein to mean “serving as an example, instance, orillustration.” Any implementation, embodiment, or feature describedherein as “exemplary,” “example,” or “illustrative,” is not necessarilyto be construed as preferred or advantageous over other implementations,embodiments, or features. Further, the implementations and embodimentsdescribed herein are not meant to be limiting. It will be readilyunderstood that certain aspects of the disclosed devices, systems, andmethods can be arranged and combined in a wide variety of differentconfigurations, all of which are contemplated herein. Additionally, thefollowing detailed description describes various features and functionsof the disclosure with reference to the accompanying Figures. In theFigures, similar symbols typically identify similar components, unlesscontext dictates otherwise.

I. Overview

As explained above, various types of robotic devices are being createdfor performing a variety of tasks that may assist users. For example, arobotic device may interact with objects while performing an assignedtask. The tools that a robotic device may use to interact with objectsare defined as end-of-arm tooling (EOAT). In particular, the roboticdevice may include a tool or an “end effector.” In an example, an endeffector may be a gripper which includes fingers that may be used tograsp and manipulate objects.

Generally, fingers are attached to actuators in an end effector, so asto allow the fingers to perform opening and/or gripping operations.Preferably, the fingers are securely coupled to the actuators via aretainer mechanism; however, a crash or other unintended outside forceacting on a rigidly coupled retainer mechanism can be problematic. Inthe case of a side force acting on a finger (e.g., a force acting at anorthogonal or oblique angle to the normal movement direction of thefinger during operation), the finger, actuator, end effector, or acoupling mechanism between the finger and actuator, may be damaged. Thesame damage may also occur in a retainer mechanism coupling otherrobotic appendages together when an unintended side force acts on one ofthe appendages. Therefore, it is beneficial to have a retainer mechanismthat securely couples two appendages (e.g., a finger and an actuator),but allows for decoupling in the event of an unintended side force thatis above a threshold that would otherwise damage a component.

Disclosed herein are retainer mechanisms with mating revolved dovetailsthat can be tuned to decouple when subject to a force or moment,particularly a side force or moment, above a threshold value. The matingdovetails may be coupled to each other by sliding the revolved maledovetail into the revolved female dovetail along an arc. Further, abackstop may positively locate one dovetail at the end of its movementalong the arc and a detent may inhibit movement of one dovetail relativeto the other along the arc during normal operation. The retainermechanism allows for easy interchangeability of appendages (includingfingers) while acting as a reusable mechanical fuse that prevents damageto an appendage from unintended side forces.

II. Example Robotic Systems

FIG. 1 illustrates an example configuration of a robotic system that maybe used in connection with the implementations described herein. Therobotic system 100 may be configured to operate autonomously,semi-autonomously, and/or using directions provided by user(s). Therobotic system 100 may be implemented in various forms, such as arobotic arm, industrial robot, or some other arrangement. Furthermore,the robotic system 100 may also be referred to as a robot, roboticdevice, or mobile robot, among other designations.

As shown in FIG. 1, the robotic system 100 may include processor(s) 102,data storage 104, and controller(s) 108, which together may be part of acontrol system 118. The robotic system 100 may also include sensor(s)112, power source(s) 114, mechanical components 110, and electricalcomponents 116. Nonetheless, the robotic system 100 is shown forillustrative purposes, and may include more or fewer components. Thevarious components of robotic system 100 may be connected in any manner,including wired or wireless connections. Further, in some examples,components of the robotic system 100 may be distributed among multiplephysical entities rather than a single physical entity. Other exampleillustrations of robotic system 100 may exist as well.

Processor(s) 102 may operate as one or more general-purpose hardwareprocessors or special purpose hardware processors (e.g., digital signalprocessors, application specific integrated circuits, etc.). Theprocessor(s) 102 may be configured to execute computer-readable programinstructions 106, and manipulate data 107, both of which are stored inthe data storage 104. The processor(s) 102 may also directly orindirectly interact with other components of the robotic system 100,such as sensor(s) 112, power source(s) 114, mechanical components 110,and/or electrical components 116.

The data storage 104 may be one or more types of hardware memory. Forexample, the data storage 104 may include or take the form of one ormore computer-readable storage media that can be read or accessed byprocessor(s) 102. The one or more computer-readable storage media caninclude volatile and/or non-volatile storage components, such asoptical, magnetic, organic, or another type of memory or storage, whichcan be integrated in whole or in part with processor(s) 102. In someimplementations, the data storage 104 can be a single physical device.In other implementations, the data storage 104 can be implemented usingtwo or more physical devices, which may communicate with one another viawired or wireless communication. As noted previously, the data storage104 may include the computer-readable program instructions 106 and thedata 107. The data 107 may be any type of data, such as configurationdata, sensor data, and/or diagnostic data, among other possibilities.

In an example, the data storage 104 may be a remote server (e.g., cloudserver) in which the robotic device 100 may store data 107. The roboticdevice may also retrieve the data 107 from the remote server. The servermay include one or more servers, such as one or more of a communicationsserver, an application server, a file server, a database server, and aweb server. A server may be referred to as a “computer server.” The datatransfer between the robotic device 100 and the cloud server may bearranged according to a file transfer protocol (FTP), or according toanother protocol.

The controller 108 may include one or more electrical circuits, units ofdigital logic, computer chips, and/or microprocessors that areconfigured to (perhaps among other tasks), interface between anycombination of the mechanical components 110, the sensor(s) 112, thepower source(s) 114, the electrical components 116, the control system118, and/or a user of the robotic system 100. In some implementations,the controller 108 may be a purpose-built embedded device for performingspecific operations with one or more subsystems of the robotic device100.

The control system 118 may monitor and physically change the operatingconditions of the robotic system 100. In doing so, the control system118 may serve as a link between portions of the robotic system 100, suchas between mechanical components 110 and/or electrical components 116.In some instances, the control system 118 may serve as an interfacebetween the robotic system 100 and another computing device. Further,the control system 118 may serve as an interface between the roboticsystem 100 and a user. The instance, the control system 118 may includevarious components for communicating with the robotic system 100,including a joystick, buttons, and/or ports, etc. The example interfacesand communications noted above may be implemented via a wired orwireless connection, or both. The control system 118 may perform otheroperations for the robotic system 100 as well.

During operation, the control system 118 may communicate with othersystems of the robotic system 100 via wired or wireless connections, andmay further be configured to communicate with one or more users of therobot. As one possible illustration, the control system 118 may receivean input (e.g., from a user or from another robot) indicating aninstruction to perform a particular gait in a particular direction, andat a particular speed. A gait is a pattern of movement of the limbs ofan animal, robot, or other mechanical structure.

Based on this input, the control system 118 may perform operations tocause the robotic device 100 to move according to the requested gait. Asanother illustration, a control system may receive an input indicatingan instruction to move to a particular geographical location. Inresponse, the control system 118 (perhaps with the assistance of othercomponents or systems) may determine a direction, speed, and/or gaitbased on the environment through which the robotic system 100 is movingen route to the geographical location.

Operations of the control system 118 may be carried out by theprocessor(s) 102. Alternatively, these operations may be carried out bythe controller 108, or a combination of the processor(s) 102 and thecontroller 108. In some implementations, the control system 118 maypartially or wholly reside on a device other than the robotic system100, and therefore may at least in part control the robotic system 100remotely.

Mechanical components 110 represent hardware of the robotic system 100that may enable the robotic system 100 to perform physical operations.As a few examples, the robotic system 100 may include physical memberssuch as leg(s), arm(s), wheel(s), hand(s), finger(s), feet, preshapercomponents, and/or end effectors. The physical members or other parts ofrobotic system 100 may further include actuators arranged to move thephysical members in relation to one another. The robotic system 100 mayalso include one or more structured bodies for housing the controlsystem 118 and/or other components, and may further include other typesof mechanical components. The particular mechanical components 110 usedin a given robot may vary based on the design of the robot, and may alsobe based on the operations and/or tasks the robot may be configured toperform.

In some examples, the mechanical components 110 may include one or moreremovable components. The robotic system 100 may be configured to addand/or remove such removable components, which may involve assistancefrom a user and/or another robot. For example, the robotic system 100may be configured with removable arms, hands, feet, and/or legs, so thatthese appendages can be replaced or changed as needed or desired. Insome implementations, the robotic system 100 may include one or moreremovable and/or replaceable battery units or sensors. In otherimplementations, the robotic system 100 may include one or moredetachable fingers. Other types of removable components may be includedwithin some implementations.

The robotic system 100 may include sensor(s) 112 arranged to senseaspects of the robotic system 100. The sensor(s) 112 may include one ormore force sensors, force/torque sensors, velocity sensors, accelerationsensors, position sensors, proximity sensors, motion sensors, locationsensors, load sensors, temperature sensors, touch sensors, depthsensors, ultrasonic range sensors, infrared sensors, object sensors,and/or cameras, among other possibilities. Within some examples, therobotic system 100 may be configured to receive sensor data from sensorsthat are physically separated from the robot (e.g., sensors that arepositioned on other robots or located within the environment in whichthe robot is operating).

The sensor(s) 112 may provide sensor data to the processor(s) 102(perhaps by way of data 107) to allow for interaction of the roboticsystem 100 with its environment, as well as monitoring of the operationof the robotic system 100. The sensor data may be used in evaluation ofvarious factors for activation, movement, and deactivation of mechanicalcomponents 110 and electrical components 116 by control system 118. Forexample, the sensor(s) 112 may capture data corresponding to the terrainof the environment or location of nearby objects, which may assist withenvironment recognition and navigation. In an example configuration,sensor(s) 112 may include RADAR (e.g., for long-range object detection,distance determination, and/or speed determination), LIDAR (e.g., forshort-range object detection, distance determination, and/or speeddetermination), SONAR (e.g., for underwater object detection, distancedetermination, and/or speed determination), VICON® (e.g., for motioncapture), one or more cameras (e.g., stereoscopic cameras for 3Dvision), a global positioning system (GPS) transceiver, and/or othersensors for capturing information of the environment in which therobotic system 100 is operating. The sensor(s) 112 may monitor theenvironment in real time, and detect obstacles, elements of the terrain,weather conditions, temperature, and/or other aspects of theenvironment. In another example, sensor(s) 112 may capture datacorresponding to one or more characteristics of a target or identifiedobject, such as a size, shape, profile, structure, or orientation of theobject.

Further, the robotic system 100 may include sensor(s) 112 configured toreceive information indicative of the state of the robotic system 100,including sensor(s) 112 that may monitor the state of the variouscomponents of the robotic system 100. The sensor(s) 112 may measureactivity of systems of the robotic system 100 and receive informationbased on the operation of the various features of the robotic system100, such as the operation of extendable legs, arms, or other mechanicaland/or electrical features of the robotic system 100. The data providedby the sensor(s) 112 may enable the control system 118 to determineerrors in operation as well as monitor overall operation of componentsof the robotic system 100.

As an example, the robotic system 100 may use force sensors to measureload on various components of the robotic system 100. In someimplementations, the robotic system 100 may include one or more forcesensors on an arm, leg, hand, foot, or finger to measure the load on theactuators that move one or more members of the arm, leg, hand, foot, orfinger. As another example, the robotic system 100 may use one or moreposition sensors to sense the position of the actuators of the roboticsystem. For instance, such position sensors may sense states ofextension, retraction, positioning, or rotation of the actuators onarms, legs, hands, feet, fingers, preshaper components, or endeffectors.

As another example, the sensor(s) 112 may include one or more velocityand/or acceleration sensors. For instance, the sensor(s) 112 may includean inertial measurement unit (IMU). The IMU may sense velocity andacceleration in the world frame, with respect to the gravity vector. Thevelocity and acceleration sensed by the IMU may then be translated tothat of the robotic system 100 based on the location of the IMU in therobotic system 100 and the kinematics of the robotic system 100.

The robotic system 100 may include other types of sensors not explicateddiscussed herein. Additionally or alternatively, the robotic system mayuse particular sensors for purposes not enumerated herein.

The robotic system 100 may also include one or more power source(s) 114configured to supply power to various components of the robotic system100. Among other possible power systems, the robotic system 100 mayinclude a hydraulic system, electrical system, batteries, and/or othertypes of power systems (e.g., internal combustion engines, fuel cells,hamster wheels, etc.). As an example illustration, the robotic system100 may include one or more batteries configured to provide charge tocomponents of the robotic system 100. Some of the mechanical components110 and/or electrical components 116 may each connect to a differentpower source, may be powered by the same power source, or be powered bymultiple power sources.

Any type of power source may be used to power the robotic system 100,such as electrical power or a gasoline engine. Additionally oralternatively, the robotic system 100 may include a hydraulic systemconfigured to provide power to the mechanical components 110 using fluidpower. Components of the robotic system 100 may operate based onhydraulic fluid being transmitted throughout the hydraulic system tovarious hydraulic motors and hydraulic cylinders, for example. Thehydraulic system may transfer hydraulic power by way of pressurizedhydraulic fluid through tubes, flexible hoses, or other links betweencomponents of the robotic system 100. The power source(s) 114 may chargeusing various types of charging, such as wired connections to an outsidepower source, wireless charging, combustion, or other examples.

The electrical components 116 may include various mechanisms capable ofprocessing, transferring, and/or providing electrical charge or electricsignals. Among possible examples, the electrical components 116 mayinclude electrical wires, circuitry, and/or wireless communicationtransmitters and receivers to enable operations of the robotic system100. The electrical components 116 may interwork with the mechanicalcomponents 110 to enable the robotic system 100 to perform variousoperations. The electrical components 116 may be configured to providepower from the power source(s) 114 to the various mechanical components110, for example. Further, the robotic system 100 may include electricmotors. Other examples of electrical components 116 may exist as well.

Although not shown in FIG. 1, the robotic system 100 may include a body,which may connect to or house appendages and components of the roboticsystem. As such, the structure of the body may vary within examples andmay further depend on particular operations that a given robot may havebeen designed to perform. For example, a robot developed to carry heavyloads may have a wide body that enables placement of the load.Similarly, a robot designed to reach high speeds may have a narrow,small body that does not have substantial weight. Further, the bodyand/or the other components may be developed using various types ofmaterials, such as metals or plastics. Within other examples, a robotmay have a body with a different structure or made of various types ofmaterials.

The body and/or the other components may include or carry the sensor(s)112. These sensors may be positioned in various locations on the roboticdevice 100, such as on the body and/or on one or more of the appendages,among other examples.

On its body, the robotic device 100 may carry a load, such as a type ofcargo that is to be transported. The load may also represent externalbatteries or other types of power sources (e.g., solar panels) that therobotic device 100 may utilize. Carrying the load represents one exampleuse for which the robotic device 100 may be configured, but the roboticdevice 100 may be configured to perform other operations as well.

As noted above, the robotic system 100 may include various types oflegs, arms, wheels, end effectors, gripping devices and so on. Ingeneral, the robotic system 100 may be configured with zero or morelegs. An implementation of the robotic system with zero legs may includewheels, treads, or some other form of locomotion. An implementation ofthe robotic system with two legs may be referred to as a biped, and animplementation with four legs may be referred as a quadruped.Implementations with six or eight legs are also possible. For purposesof illustration, robotic arm implementations of the robotic system 100are described below.

FIG. 2 shows an example robotic arm 200. As shown, the robotic arm 200includes a base 202, which may be a stationary base or may be a movablebase. In the case of a movable base, the base 202 may be considered asone of the mechanical components 110 and may include wheels (not shown),powered by one or more of actuators, which allow for mobility of theentire robotic arm 200.

Additionally, the robotic arm 200 includes joints 204A-204F each coupledto one or more actuators. The actuators in joints 204A-204F may operateto cause movement of various mechanical components 110 such asappendages 206A-206F and/or end effector 208 (which may be consideredone or more appendages). For example, the actuator in joint 204F maycause movement of appendage 206F and end effector 208 (i.e., since endeffector 208 is coupled to appendage 206F). Further, end effector 208may take on various forms and may include various parts. In one example,end effector 208 may take the form of a gripper such as a finger gripperas shown here or a different type of gripper such as a suction gripper.In another example, end effector 208 may take the form of a tool such asa drill or a brush. In yet another example, the end effector may includesensors such as force sensors, location sensors, and/or proximitysensors. Note that the end effector 208 may be a detachable end effectorsuch that the robotic arm 200 may swap out the end effector 208 with adifferent end effector. Other examples may also be possible.

In an example implementation, a robotic system 100, such as robotic arm200, may be capable of operating in a teach mode. In particular, teachmode may be an operating mode of the robotic arm 200 that allows a userto physically interact with and guide the robotic arm 200 towardscarrying out and recording various movements. In a teaching mode, anexternal force is applied (e.g., by the user) to the robotic system 100based on a teaching input that is intended to teach the robotic systemregarding how to carry out a specific task. The robotic arm 200 may thusobtain data regarding how to carry out the specific task based oninstructions and guidance from the user. Such data may relate to aplurality of configurations of the mechanical components 110, jointposition data, velocity data, acceleration data, force/torque data,force data, and power data, among other possibilities.

For example, during teach mode the user may grasp onto any part of therobotic arm 200 and provide an external force by physically moving therobotic arm 200. In particular, the user may guide the robotic arm 200towards grasping onto an object and then moving the object from a firstlocation to a second location. As the user guides the robotic arm 200during teach mode, the system may obtain and record data related to themovement such that the robotic arm 200 may be configured toindependently carry out the task at a future time during independentoperation (e.g., when the robotic arm 200 operates independently outsideof teach mode). Note, however, that external forces may also be appliedby other entities in the physical workspace such as by other objects,machines, and/or robotic systems, among other possibilities.

III. Example Reusable Mechanically Fused Dovetail Retainer Mechanisms

As noted above, the present disclosure includes implementations thatrelate to a retainer mechanism. The retainer mechanism may be used in arobotic device and/or system to allow easy appendage and finger changes,while protecting against catastrophic damage to the robotic device dueto unintended impacts or loads.

FIG. 3 illustrates an example gripper 300, according to an exampleembodiment. Gripper 300 may be deployed in place of end effector 208 inrobotic arm 200 and/or as one of the mechanical components 110 inrobotic system 100. Gripper 300 includes two opposable fingers 304,though more or fewer fingers are contemplated.

Gripper 300 includes an actuator base 302, according to an exemplaryembodiment. A retainer mechanism 400 may be used to attach each of oneor more fingers 304 to one or more actuators 310 in the actuator base302. For purposes of illustration, a normal rotational (ortranslational) movement of a finger 304 is shown by arrow 308.Additionally, a side force 306 is represented acting against the finger304 orthogonally to the normal movement 308 (i.e., into the Figure). Theside force 306 may be a component of a force acting on the fingerobliquely to the normal movement 308.

FIG. 4A-K illustrate an example retainer mechanism 400 and itscomponents, according to an exemplary embodiment. Although thecomponents illustrated in FIGS. 4A-K are shown with certain designfeatures and/or orientations, it should be understood that one or morefeatures may be removed, added, and/or modified while remaining withinthe scope of this disclosure. Also, the orientation and combination offeatures may be changed based on the desired implementation.

Retainer mechanism 400 includes a first member 402 and a second member404. Each member 402 and 404 may be fixedly connected to a respectiveappendage. For example, in a preferred arrangement, first member 402 maybe connected to a finger, such as finger 304 and second member 404 maybe connected to an actuator, such as an actuator in actuator base 302.Alternatively, in another arrangement, first member 402 may be connectedto an actuator, such as an actuator in actuator base 302 and secondmember 404 may be connected to a finger, such as finger 304.Alternatively, retainer mechanism 400 may be connected between otherappendages, such as at joints 204A-F in system 200.

First member 402 includes a body 403 with a male dovetail 408 extendingdownward from the body. The length of male dovetail 408 along its outersurfaces 408A is not linear, but rather is revolved about a central axis401 and takes the form of an arc. The male dovetail 408 further includesan inner channel 426 between the outer surfaces 408. The inner channel426 permits greater deflection of the outer surfaces 408A in response toa side-loading force than if the male dovetail 408 was entirely solidbetween the outer surfaces 408A.

First member 402 further includes a pair of wings 412 that extendoutward from the body 403. As illustrated in this example embodiment,the each wing 412 is adjacent to a corresponding outer surface 408A ofthe male dovetail 408. Each wing 412 may extend orthogonally from thebody and at an acute angle relative to its respective male dovetailouter surface 408A. However, in another implementation, each wing 412may be at an orthogonal or obtuse angle to its respective outer surface408A.

As illustrated in this example, second member 404 includes two halves404A and 404B, though in another embodiment, second member 404 may beunitary. Constructing second member 404 out of halves 404A and 404Bprovides benefits in the manufacture of the second member 404, includingeasier mold release, machining, or 3D printing, depending on themethod(s) of manufacture. In the illustrated example, halves 404A and404B are secured together with fasteners 416 through thru-holes 418A and418B. The fasteners 416 may be, for example, screws, bolts, or rivets.Alternatively, the halves 404A and 404B may be fastened together byother means, including, for example, adhesives, plastic welding methods,and/or latch geometries.

Second member 404 includes a female dovetail 410 extending upward from abody 405. Similar to male dovetail 408, the length of female dovetail410 along its inner surfaces 410A is not linear, but rather is revolvedabout the central axis 401 and takes the form of an arc. The innersurfaces 410A define two sides of a channel 411 between inner surfaces410A, with a third side of the channel 411 defined by a base surface420. The base surface 420 is similarly revolved about the central axis401 and takes the form of an arc.

First member 402 may be slidably engaged with second member 404, asdepicted in stepwise manner in FIGS. 5A-5C. An end of male dovetail 408of first member 402 may be inserted into an end of female dovetail 410of second member 404. Then, first member 402 may be slid further intosecond member 404 in a rotational manner along an arc about central axis401 (central axis 401 is illustrated in FIGS. 4A and 4B). The firstmember 402 may slide into second member 404 until it hits a backstopand/or detent.

Referring back to FIGS. 4A-K, second member 404 includes a backstop 406,which extends outward from the second body 405. As the first member 402is inserted into the second member 404, the backstop 406 eventuallymakes contact with an end of the male dovetail 408 and preventsrotational movement of the first member 402 relative to the secondmember 404 about the central axis 401 beyond the backstop 406.

The female dovetail 410 includes a top surface 421 adjacent to eachcorresponding inner surface 410A. Each top surface 421 may extend at anacute, orthogonal, or obtuse angle relative to its respective femaledovetail inner surface 418A. Preferably, each top surface 421 isoriented concentric to a corresponding wing 412, such that, when thesecond member 404 is coupled to with the first member 402, each topsurface 421 has a mating interface with the corresponding wing 412.

Similarly, the male dovetail 408 includes two bottom surfaces 428, eachadjacent to a corresponding outer surface 408A. Each bottom surface 428may extend at an acute, orthogonal, or obtuse angle relative to itsrespective outer surface 418A. Preferably, each bottom surface 428 isoriented concentric to the base surface 420, such that, when the secondmember 404 is coupled with the first member 402, each bottom surface 428has a mating interface with the base surface 420.

One or more detents may be included at any of these mating surfaces toinhibit rotational movement of first member 402 relative to secondmember 404. The detent can prevent the first member 402 from slidingback out of the second member 404 by providing a securing force thatinhibits relative movement about the central axis 401. As shown in theexample embodiment in FIGS. 4A-K, a detent 414 is located near an end ofthe female dovetail 410 and an end of the wings 412. Each wing 412includes a recess 414B of the detent 414 that is configured to mate witha protrusion 414A of the detent 414 on the top surfaces 410A. When thefirst member 402 is slid into the second member 404 and up against thebackstop 406, the protrusion 414A “clicks” into the recess 414B andprevents the first member 402 from sliding back out of the second member404, unless sufficient force is applied to “unclick” the detent 414. Asillustrated, the recess 414B is a groove and the protrusion 414A is alinear protrusion. However, other embodiments are possible, such as ahemispherical or conical recess and protrusion. Other detent designs mayprovide even greater securing power, such as a square recess andprotrusion, or a French cleat design, and are also contemplated herein.Further, the protrusion and recess locations may be reversed. Forexample a wing 412 may have a protrusion and a top surface 410A may havea recess. And in other embodiments, one or more detents may be locatedadditionally or alternatively at other locations. FIGS. 12 and 13illustrate some alternative locations for a recess/protrusion detentsimilar to detent 414. For example, a detent may be provided at themating interface between the base surface 420 and the bottom surface(s)428 at the locations 1204A and 1204B, respectively. In another example,a detent may be provided at the mating interface between the femaledovetail inner surface(s) 410A and the male dovetail outer surface(s)408A at the locations 1202A and 1202B, respectively. It should be notedthat a detent on the dovetail outer and inner surface(s) 408A and 410Amay affect the decoupling force of the retainer mechanism embodimentsdisclosed herein.

Returning to other features of retainer mechanism 400, FIGS. 4A-Kfurther illustrate that the male dovetail 408 further includes a lead-infeature 424, here depicted as a tapered transition between an outersurface 408A and an end of the male dovetail 408. Similarly femaledovetail 418 also includes a lead-in feature 422, here depicted as atapered transition between an inner surface 408A and an end of thefemale dovetail 410 The lead-in features 422 and 424 permit easierlocation of the first member 402 to the second member 404 when they areinitially slidably engaged, such as in FIGS. 5A to 5B.

FIG. 6 illustrates a retainer mechanism during side-force decoupling,and illustrates an application of its use. In an embodiment with afinger and an actuator, a finger 601 may be coupled to an actuator 609via the retainer mechanism 600. Retainer mechanism 600 may be the sameas, or similar to, retainer mechanism 400, and includes a finger mount602 and an actuator mount 604, which may correspond to first member 402and second member 404, respectively. In an alternative embodiment,finger mount 602 could instead take the form of second member 404 (i.e.,a female revolved dovetail) and actuator mount 604 could instead takethe form of first member 402 (i.e., a male revolved dovetail)

In the illustrated example, when a side force 607 is applied to thefinger 601, the retainer 600 is able to decouple instead of breaking.One of the wings 612 may elastically deform to allow rotation of fingermount 602 relative to the actuator mount 604 in the direction of theside force 607. The male dovetail 608, which kept the finger mount 602securely coupled to the actuator mount 604 via the female dovetail,begins to controllably decouple. In this example, the root widths(described below with respect to FIG. 7) of female dovetail 610 aresignificantly wider than the root widths of male dovetail 608. Assumingfemale dovetail 610 and male dovetail 608 are constructed of similarmaterials, male dovetail portion 608A will elastically deform and bendinto the inner channel 626, allowing the male dovetail 608 to pop out ofthe female dovetail 610. In other embodiments, where female dovetail 610is made of a softer material or has a narrower root width than maledovetail 608, a portion of the female dovetail 610 may elasticallydeform and allow a similar decoupling action. In another embodiment,where the materials are similar and the root widths are similar, one ormore portions of both male dovetail 608 and female dovetail 610 mayelastically deform to allow the decoupling. Because the dovetails 608and/or 610 elastically deformed, they will return substantially orcompletely to their original shape and may be reused and recoupled witheach other, such as in the illustration in FIGS. 5A-C.

FIG. 7 illustrates reference dimensions of a retainer mechanism 700,according to an example implementation. Retainer mechanism 700 may bethe same as, or similar to, retainer mechanisms 400 and/or 600, or otherembodiments disclosed herein. FIG. 7 illustrates portions of a firstmember 702 and a second member 704, whose features, such as male andfemale dovetails and inner channels, correspond to similar featuresdescribed in other embodiments disclosed herein.

The male dovetail of first member 702 can be defined in part by a maleroot width 706, a male dovetail height 708, and a male dovetail angle710 which is measured from an imaginary vertical plane, as is commonpractice. The female dovetail of second member 704 can be defined inpart by a female root width 716, a female dovetail height 718, and afemale dovetail angle 720 which is also measured from an imaginaryvertical plane. At the mating interface between an outer surface of themale dovetail and the inner surface of a female dovetail, the dovetailswill overlap by the overlap width 722, as measured from the location ofthe respective root widths. The male dovetail inner channel may bedefined in part by channel width 712 and channel height 714.

To tune the “fuse-out” force (i.e., a side-load force sufficient tocause decoupling) and deformation characteristics associated withdecoupling a retainer mechanism, the root widths 706 and 716, overlap722, root heights 708 and 718, angles 710 and 720, and inner channelwidth and height 712 and 714 can be modified to achieve a desiredbalance of fuse-out force, elastic versus plastic deformation, andretention force in directions essential to normal operations of anappendage (e.g. a finger). In a preferred embodiment, angles 710 and 720are substantially identical, but they may be different in alternativeembodiments. Also in preferred embodiments, the root width 706 issubstantially the same as the root width 716.

FIG. 8 is a chart illustrating root width versus fuse-out force andsafety factor, according to an example implementation. Empirical datadeveloped from modeling and testing embodiments of the retentionmechanisms disclosed herein show that, given a constant overlap width,fuse-out force increases as a given root width widens, as illustrated bythe dashed line in FIG. 8. The empirical data shows the same correlationwhether the male root width (e.g., root width 706) or the female rootwidth (e.g., root width 716) is considered. Therefore, if a givenoverlap and fuse-out force is desired, then a root width can bedetermined. Similarly, if design constraints dictate a given root widthand overlap, then fuse-out force can be calculated.

Similarly obtained empirical data also show that the safety factordecreases as a given root width increases. Safety factor is the yieldstress of the material divided by the stress level at the maximum stresslocation/condition. It is preferred to have the largest safety factorpossible; however, increasing the safety factor beyond a certain pointgenerally adds detrimental weight and/or size. The preferred safetyfactor value is greater than 1, with some additional margin for systemvariances.

Tests and modeling were performed on a retention mechanism 400 made ofNylon 6/6. For a gripper design similar to gripper 300, a desiredfuse-out force F₁ was set at 5 lbs. Male and female dovetail heightswere set to 4 mm and the overlap width between the dovetails was set to1 mm. Male and female root widths were tested at different widths, butin each case were set equivalent to each other. It was determinedthrough modeling and quantitative testing that a root width W₁ of 3 mmfor both male and female root widths together resulted in the desiredfuse-out force of 5 lbs and an acceptable safety factor S₁ of 1.2. Usingless than the 3 mm determined root width W₁ would result in a lowerfuse-out force and a higher safety factor. Correspondingly, using morethan the 3 mm determined root width W₁ would result in a higher fuse-outforce and a lower safety factor. Increasing overlap width (e.g., bychanging the dovetail angle) can also increase fuse-out force anddecrease the safety factor, and vice-versa. Similarly, modifying theroot dovetail heights can also change the fuse-out force and safetyfactors.

Failing to maintain an adequate safety factor or an appropriate fuse-outforce can result in plastic deformation of the retention mechanism,particularly during the first few fuse-out cycles. FIG. 9 is a chartillustrating fuse-out force versus fuse-out cycles, according to anexample implementation. A non-optimized retention mechanism similar toretention mechanism 400 was tested for fuse-out force over repeatedfuse-out (decoupling) cycles. The non-optimized retention mechanism wassimilarly sized in overall dimensions to retention mechanism 400, butwithout an inner channel opening at each of the male dovetail and withreference dimensions different than those described immediately above.The non-optimized retention mechanism exhibited continuing plasticdeformation on the outer sides of the male dovetail after each of thefour initial fuse-out cycles. As a result, the fuse-out force decreaseddramatically over the initial fuse-out cycles before reaching asubstantially steady-state value for the remaining fuse-out cycles, asillustrated by the dashed line in FIG. 9. Such variable fuse-out forceis undesirable because it doesn't allow for consistent operatingconditions and function, and prevents re-usability of a consistentlyperforming retention mechanism. Also, plastic deformation from fuse-outmay negatively affect reassembly. Consequently, a retention mechanism400 configured with the reference dimensions determined above wastested. While the overall fuse-out force of retention mechanism 400 waslower, the fuse-out force was substantially consistent across allcycles, with only negligible reduction in fuse-out force after the firstcycle, as illustrated by the solid line FIG. 9. Consequently, theretention mechanism 400, as tested, would be re-useable over many cyclesbecause there is no significant degradation in performancecharacteristics.

In some cases it may be desirable to quickly adjust the fuse-out forceof a retainer mechanism, such as mechanism 400. One manner of quicklytuning the fuse-out force is by adding an insert into the inner channel426 of the male dovetail 408 to restrict the bending/deformation of themale dovetail during fuse-out decoupling. The insert can effectivelyincrease fuse-out force, with harder or larger inserts resulting inrelatively greater fuse-out force than softer or smaller inserts. FIGS.10A and 10B illustrate front and perspective views, respectively, of aretainer mechanism 1000 and insert 1001, according to an exampleimplementation. The retainer mechanism 1000 is similar to retainermechanism 400 and includes first and second mounts 1002 and 1004, withrespective revolved male and female dovetails, and an inner channel inthe male dovetail. A shaped insert 1001 is provided in the inner channelto modify the fuse-out characteristics. In the embodiment shown, theinsert 1001 is a segment of an annular ring and fills the inner channel.Other insert embodiments are also envisioned, including inserts with adifferent cross-sectional shape (e.g. trapezoidal), different heights,different widths, and/or different lengths. FIG. 11 is a chartillustrating fuse-out force versus fuse-out cycles, and comparesidentical retainer mechanisms with and without an insert, according toan example implementation. It can be seen that a retainer mechanism withan insert (solid line) will exhibit increased fuse-out force as comparedto a retainer mechanism without an insert (dashed line).

IV. Conclusion

The present disclosure is not to be limited in terms of the particularembodiments described in this application, which are intended asillustrations of various aspects. Many modifications and variations canbe made without departing from its spirit and scope, as will be apparentto those skilled in the art. Functionally equivalent methods andapparatuses within the scope of the disclosure, in addition to thoseenumerated herein, will be apparent to those skilled in the art from theforegoing descriptions. Such modifications and variations are intendedto fall within the scope of the appended claims.

The above detailed description describes various features and functionsof the disclosed systems, devices, and methods with reference to theaccompanying figures. In the figures, similar symbols typically identifysimilar components, unless context dictates otherwise. The exampleembodiments described herein and in the figures are not meant to belimiting. Other embodiments can be utilized, and other changes can bemade, without departing from the spirit or scope of the subject matterpresented herein. It will be readily understood that the aspects of thepresent disclosure, as generally described herein, and illustrated inthe figures, can be arranged, substituted, combined, separated, anddesigned in a wide variety of different configurations, all of which areexplicitly contemplated herein.

The particular arrangements shown in the figures should not be viewed aslimiting. It should be understood that other embodiments can includemore or less of each element shown in a given figure. Further, some ofthe illustrated elements can be combined or omitted. Yet further, anexample embodiment can include elements that are not illustrated in thefigures.

While various aspects and embodiments have been disclosed herein, otheraspects and embodiments will be apparent to those skilled in the art.The various aspects and embodiments disclosed herein are for purposes ofillustration and are not intended to be limiting, with the true scopebeing indicated by the following claims.

The invention claimed is:
 1. A retainer mechanism comprising: a firstmember comprising: a first body, and a male dovetail extending outwardfrom the first body, wherein the male dovetail comprises two outersurfaces inclined relative to each other, and wherein the male dovetailis arranged in an arc about a central axis; and a second membercomprising: a second body, and a female dovetail extending outward fromthe second body, the female dovetail comprising two inner surfacesinclined relative to each other, wherein the two inner surfaces define afirst channel between the two inner surfaces, wherein the femaledovetail is arranged in an arc about the central axis, and wherein thefemale dovetail is configured to couple with the male dovetail, suchthat each of the two outer surfaces of the male dovetail mates with oneof the respective inner surfaces of the female dovetail, wherein atleast a portion of the first member or second member is elasticallydeformable such that when the female dovetail is coupled to the maledovetail, the retainer mechanism is configured to allow the maledovetail to decouple from the female dovetail without breaking when anorthogonal force applied at either the first member or the second memberis more than a threshold force.
 2. The retainer mechanism of claim 1,wherein the male dovetail further comprises an inner channel locatedbetween the two outer surfaces.
 3. The retainer mechanism of claim 2,further comprising an insert located within the inner channel of themale dovetail.
 4. The retainer mechanism of claim 3, wherein the insertis arranged as a segment of an annular ring.
 5. The retainer mechanismof claim 1, wherein the first member further comprises two wingsextending outward from the first body, wherein each wing is orientedadjacent to and at an angle relative to one of the respective outersurfaces of the male dovetail, wherein each wing is arranged in an arcabout the central axis, wherein the female dovetail further comprisestwo top surfaces, wherein each top surface is oriented adjacent to andat an angle relative to one of the respective inner surface of thefemale dovetail, and wherein each of the respective top surfaces isconfigured to mate to one of the respective wings of the male dovetail.6. The retainer mechanism of claim 1, wherein the second body furthercomprises a base surface defining a side of the channel between the twoinner surfaces of the female dovetail, wherein the base surface isarranged in an arc about the central axis, wherein the male dovetailfurther comprises two bottom surfaces, wherein each bottom surface isoriented adjacent to and at an angle relative to one of the respectiveouter surface of the male dovetail, and wherein each of the respectivebottom surfaces is configured to mate to the base surface of the secondbody.
 7. The retainer mechanism of claim 1, further comprising abackstop, wherein the backstop extends outward from the second body andis configured to mate with an end of the male dovetail and preventrotational movement of the first body relative to the second body aboutthe central axis beyond the backstop.
 8. The retainer mechanism of claim1 further comprising a detent configured to inhibit rotational movementof the first body relative to the second body about the central axis. 9.The retainer mechanism of claim 8, wherein the detent comprises: arecess; and a protrusion configured to mate with the recess.
 10. Theretainer mechanism of claim 9, wherein the recess is arranged as agroove, and wherein the protrusion is arranged as a linear protrusion.11. The retainer mechanism of claim 5 further comprising a detentconfigured to inhibit rotational movement of the first body relative tothe second body about the central axis, wherein the detent is located atan interface between at least one wing of the first body and at leastone respective top surface of the female dovetail.
 12. The retainermechanism of claim 1 further comprising a detent configured to inhibitrotational movement of the first body relative to the second body aboutthe central axis, wherein the detent is located at an interface betweenat least one outer surface of the male dovetail and at least one innersurface of the female dovetail.
 13. The retainer mechanism of claim 6further comprising a detent configured to inhibit rotational movement ofthe first body relative to the second body about the central axis,wherein the detent is located at an interface between at least onebottom surface of the male dovetail and the base surface of the secondbody.
 14. A retainer mechanism comprising: a first member comprising: afirst body, and a male dovetail extending outward from the first body,wherein the male dovetail comprises: (i) two outer surfaces inclinedrelative to each other, and (ii) an inner channel located between thetwo outer surfaces, and wherein the male dovetail is arranged in an arcabout a central axis; a second member comprising; a second body, and afemale dovetail extending outward from the second body, the femaledovetail comprising two inner surfaces inclined relative to each other,wherein the two inner surfaces define a first channel between the twoinner surfaces, wherein the female dovetail is arranged in an arc aboutthe central axis, wherein the female dovetail is configured to couplewith the male dovetail, such that each of the two outer surfaces of themale dovetail mates with one of the respective inner surfaces of thefemale dovetail, wherein at least a portion of the first member orsecond member is elastically deformable such that when the femaledovetail is coupled to the male dovetail, the retainer mechanism isconfigured to allow the male dovetail to decouple from the femaledovetail without breaking when an orthogonal force applied at either thefirst member or the second member is more than a threshold force; and adetent configured to inhibit rotational movement of the first bodyrelative to the second body about the central axis.
 15. The retainermechanism of claim 14, wherein the first member further comprises twowings extending outward from the first body, wherein each wing isoriented adjacent to and at an angle relative to one of the respectiveouter surfaces of the male dovetail, wherein each wing is arranged in anarc about the central axis, wherein the female dovetail furthercomprises two top surfaces, wherein each top surface is orientedadjacent to and at an angle relative to one of the respective innersurface of the female dovetail, and wherein each of the respective topsurfaces is configured to mate to one of the respective wings of themale dovetail.